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Author

Yusuf Kalsekar

1 paper indexed here

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Sep 2026

Design and multi-domain optimisation of a fixed-wing UAV with payload deployment system

The purpose of this study is to design, analyse, fabricate and validate a fixed-wing UAV for stable low-speed flight, payload carriage and controlled in-flight deployment. It aims to achieve aerodynamic efficiency, structural safety, stability and practical manufacturability for short-range logistics, surveillance...

Aditya Sivaraman, A. Ansari, Aqleem Siddiqui et al. · 0 citations

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